Polar_diagram_of_coefficients_of_lift_and_drag_for_angles_of_attack.png
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Summary
| Description |
English:
Polar diagram of coefficients of lift (
C
L
) and drag (
C
D
) for the angles of attack shown for a hypothetical sail. The dotted line is tangential with the point of highest ratio of lift over drag (
C
L
/
C
D
). Also shown is flow status, ranging from attached to stalled.
|
| Date | |
| Source | Own work |
| Author | HopsonRoad |
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